Multi-rotor unmanned aerial vehicle with high-precision course control

Abstract

The invention discloses a multi-rotor unmanned aerial vehicle with high-precision course control, and relates to the technical field of multi-rotor unmanned aerial vehicles, the multi-rotor unmanned aerial vehicle with high-precision course control comprises a vehicle body, a mounting block, an unmanned aerial vehicle controller and a wind direction and wind force sensor; each wing comprises a connecting rod and an electric rotor wing; the adjusting assembly comprises a balance rotor wing and a cross rod; the driving assembly comprises a horizontal adjusting piece and an axial adjusting piece. According to the unmanned aerial vehicle, the wind direction and wind power changes in the flight environment can be monitored in real time, the balance rotor wing in the adjusting assembly can respond rapidly, the orientation and wind power output of the unmanned aerial vehicle are adjusted according to an instruction of the unmanned aerial vehicle controller, and therefore the unmanned aerial vehicle can be controlled in real time. Reverse wind power is generated to counteract the influence of external wind power, so that the balance state of the unmanned aerial vehicle is effectively maintained, the flight stability is improved, adverse conditions such as strong wind and crosswind are effectively handled, and the course precision of the unmanned aerial vehicle is enhanced.

Description

Technical Field

[0001] The invention relates to the technical field of multi-rotor unmanned aerial vehicles, and in particular to a multi-rotor unmanned aerial vehicle with high-precision heading control. Background Art

[0002] Multi-rotor drones generate lift thrust by rotating the motors on each axis, which drives the rotors to rotate. The total pitch of the rotors is fixed, and by changing the relative speed between different rotors, the magnitude of the single-axis propulsion force can be changed, thereby controlling the trajectory of the aircraft.

[0003] Existing multi-rotor UAVs often experience problems such as shaking and inability to hover stably during flight, especially in complex and changeable flight environments, such as strong winds, crosswinds and other adverse conditions. This not only affects the flight stability of the UAV, but also limits its application scope. At the same time, the direct impact of strong winds on the electric rotors will also increase flight resistance, reduce flight efficiency and heading accuracy, and bring challenges to the flight control of the UAV. Summary of the invention

[0004] The present invention provides a multi-rotor UAV with high-precision heading control to solve the above-mentioned problems.

[0005] To solve the above problems, the present invention provides the following technical solutions: a multi-rotor UAV with high-precision heading control, comprising: a body, the outer wall of which is symmetrically provided with a plurality of mounting blocks for mounting wings, the upper end faces of which are respectively provided with a UAV controller and a wind direction and wind force sensor, the wind direction and wind force sensor being electrically connected to the UAV controller; a wing, comprising a connecting rod connected to the mounting block and an electric rotor mounted on the upper end face of the connecting rod, the electric rotor being mounted on the upper end face of the connecting rod; an adjusting assembly, comprising a balancing rotor symmetrically arranged on the left and right and electrically connected to the UAV controller, and a cross bar mounted on the lower end face of the body, the balancing rotor being slidably connected to the cross bar, and being used to adjust the balance rotor when the wind is too strong and causes the UAV to generate When the drone shakes and cannot maintain a hovering state, the reverse wind force is generated to adjust the flight angle of the drone to maintain the balance of the drone; a driving component is arranged on the bottom surface of the fuselage and is transmission-connected to the adjustment component and electrically connected to the drone control, and includes a horizontal adjustment member and an axial adjustment member for driving the balancing rotor, thereby adjusting the direction of the balancing rotor, so that when the drone tilts or shakes violently according to the wind direction, it can be adjusted to a suitable position and angle in time, thereby generating balancing wind force through the balancing rotor to restore the stability of the drone; a wind resistance cover is installed on the upper end surface of the wing and surrounds the propeller of the wing, and is used to guide the strong wind blowing toward the wing and make it downward along the wing, thereby reducing the impact of the strong wind on the electric rotor.

[0006] As a preferred technical solution of the present invention, the upper end surface of the cross bar is provided with a through groove, and the front and rear arms of the through groove are symmetrically provided with inwardly recessed grooves. The upper end surface of the balancing rotor is provided with a slider, and the slider is slidably connected in the through groove, and a driving member is provided in the slider, and the driving member is used to drive the slider to slide in the through groove.

[0007] As a preferred technical solution of the present invention, the upper and lower walls in the groove are provided with staggered racks, the driving member includes a dual-axis motor and a first gear meshing with the racks, an installation bin is provided in the slider, the dual-axis motor is installed in the installation bin, the output end of the dual-axis motor passes through the installation bin and extends into the groove, the first gear is installed at the output end of the dual-axis motor and meshes with the racks, and an integrally formed L-shaped plate is symmetrically provided on the upper end surface of the slider, and the slider is slidably connected to the outer wall of the cross bar through the L-shaped plate.

[0008] As a preferred technical solution of the present invention, the horizontal adjustment member includes a sleeve, a connecting plate, a mounting column, a mounting cylinder and a first motor. The first motor is fixedly installed on the bottom surface of the machine body, and the output shaft of the first motor is set downward. The sleeve is installed on the bottom surface of the machine body and covers the first motor. A bearing is installed in the sleeve, and the mounting cylinder is installed in the bearing. The connecting plate is fixedly installed on the outer wall of the mounting cylinder. The mounting column is symmetrically installed on the bottom surface of the connecting plate. The left end face of the mounting column is provided with a through hole, and a rotating shaft is rotatably connected in the through hole. The rotating shaft is fixedly connected to the cross bar, and the other end of the rotating shaft is connected to the axial adjustment member, and the axial adjustment member is installed in the mounting cylinder.

[0009] As a preferred technical solution of the present invention, the axial adjustment member includes a mounting plate, a connecting member and a second motor. The mounting plate is installed on the inner wall of the mounting cylinder. The connecting member is arranged on the right end face of the mounting plate and is respectively connected to symmetrically arranged rotating shafts for transmitting power to make the left and right symmetrical cross bars rotate and adjust simultaneously. The second motor is connected to the connecting member.

[0010] As a preferred technical solution of the present invention, the connecting member includes a mounting seat, a second gear, a third gear and a connecting shaft, the mounting seat is installed on the right end face of the mounting plate, the second gear is connected to the mounting seat for front-to-back symmetrical rotation, the third gear is connected to the mounting seat for left-to-right symmetrical rotation, and the second gear and the third gear are meshed with each other, the connecting shaft is respectively connected to the outer wall of the symmetrical second gear, the rotating shaft extends into the mounting cylinder and is rotatably connected to the connecting shaft, and the second motor is fixedly connected to one of the third gears.

[0011] As a preferred technical solution of the present invention, the wind resistance cover includes a blocking cylinder and cylindrical fan blades, a connecting plate is symmetrically arranged inside the blocking cylinder, the connecting plate is fixedly connected to the outer wall of the connecting rod, the outer wall of the blocking cylinder is provided with a plurality of wind guide grooves penetrating downwardly through the blocking cylinder, and the cylindrical fan blades are rotatably connected to the outer wall of the blocking cylinder.

[0012] As a preferred technical solution of the present invention, the cylindrical fan blades include a plurality of inclined blades and mounting rings symmetrically arranged up and down, the mounting rings are rotatably connected to the outer wall of the blocking cylinder, and the blades are installed between the mounting rings symmetrically arranged up and down.

[0013] As a preferred technical solution of the present invention, the air guide grooves are spirally distributed on the outer wall of the blocking cylinder.

[0014] Compared with the prior art, the present invention provides a multi-rotor UAV with high-precision heading control, which has the following beneficial effects: 1. The multi-rotor UAV with high-precision heading control can monitor the wind direction and wind force changes in the flight environment in real time by setting wind force, wind direction and wind force sensors, adjustment components, drive components and wind resistance covers, and provide accurate data support for the flight control of the UAV. When encountering strong winds or sudden changes in wind direction that cause the UAV to shake and cannot hover stably, the balance rotor in the adjustment component can respond quickly, adjust its direction and wind force output according to the instructions of the UAV controller, and generate reverse wind force to offset the influence of external wind force, thereby effectively maintaining the balance state of the UAV and improving flight stability. The flexible adjustment mechanism of the balance rotor enables the UAV to quickly adjust its flight attitude when facing a complex and changeable flight environment, effectively cope with adverse conditions such as strong winds and side winds, and enhance the UAV's wind resistance and environmental adaptability. The wind resistance cover further reduces the direct impact of strong winds on the electric rotors, and effectively reduces wind resistance by guiding the airflow to flow downward along the wings, thereby improving the flight efficiency and heading accuracy of the UAV.

[0015] 2. The balancing rotor in the present invention is slidably connected to the through groove on the cross bar through the slider, and a driving member is provided in the slider, which can flexibly adjust the position and angle of the balancing rotor. When the UAV encounters strong winds or sudden changes in wind direction, the balancing rotor can respond quickly and offset the influence of external wind force by generating reverse wind force, thereby effectively maintaining the balance of the UAV and significantly improving flight stability. The driving member in the slider adopts a dual-axis motor and a first gear design meshing with the rack, which realizes precise control of the sliding of the slider.

[0016] 3. By setting up horizontal adjustment parts and axial adjustment parts, the balancing rotor can not only be flexibly adjusted in the horizontal direction, but also can be precisely adjusted in the axial direction. This dual-axis adjustment mechanism enables the UAV to adjust its flight attitude and heading in real time according to changes in wind direction and wind force during flight, further improving the accuracy and stability of heading control.

[0017] 4. The wind resistance cover design of the present invention effectively reduces the direct impact of strong wind on the electric rotor through the blocking cylinder and cylindrical fan blades. The blocking cylinder, as the main windproof structure, can absorb and disperse part of the wind force, and the rotation of the cylindrical fan blades can further guide the airflow, reduce the impact of wind resistance and turbulence on the UAV, thereby significantly improving the flight stability of the UAV. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 It is a schematic diagram of the external structure of the present invention; Figure 2 It is a schematic diagram of the external structure of the machine body of the present invention; Figure 3 This is a schematic diagram of the external structure of the present invention from another angle; Figure 4 is a cross-sectional view of a drive assembly and an adjustment assembly of the present invention; Figure 5 It is a cross-sectional view of the axial adjustment member of the present invention; Figure 6 It is a cross-sectional view of the slider and the driving member of the present invention; Figure 7 This is an exploded view of the wind resistance cover of the present invention; Figure 8 The present invention provides Figure 4 A schematic diagram of the enlarged structure of part a; Fig. 9 The present invention provides Figure 4 Schematic diagram of the enlarged structure of part b.

[0019] In the figure: 1, fuselage; 11, mounting block; 12, drone controller; 13, wind direction and wind force sensor; 2, wing; 21, connecting rod; 22, electric rotor; 3, adjustment assembly; 31, balance rotor; 311, slider; 312, L-shaped plate; 313, mounting compartment; 32, cross bar; 321, through slot; 322, groove; 323, rack; 33, driving member; 331, dual-axis motor; 332, first gear; 4, driving assembly; 41, horizontal adjustment member; 411, sleeve; 41 2. Connecting plate; 413. Mounting column; 414. Mounting cylinder; 415. First motor; 416. Through hole; 417. Rotating shaft; 418. Bearing; 42. Axial adjustment member; 421. Mounting plate; 422. Connecting member; 423. Second motor; 424. Mounting seat; 425. Second gear; 426. Third gear; 427. Connecting shaft; 5. Wind resistance cover; 51. Blocking cylinder; 511. Connecting plate; 512. Wind guide groove; 52. Cylindrical fan blade; 521. Mounting ring; 522. Blade. DETAILED DESCRIPTION

[0020] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0021] See also Figure 1 - Fig. 9The present invention discloses a multi-rotor UAV with high-precision heading control, comprising a body 1, wings 2, an adjustment component 3, a drive component 4 and a wind resistance cover 5, wherein the body 1 has a plurality of mounting blocks 11 symmetrically arranged on its outer wall for mounting the wings 2, and a UAV controller 12 and a wind direction and wind force sensor 13 are respectively arranged on its upper end surface, and the wind direction and wind force sensor 13 is electrically connected to the UAV controller 12; the wing 2 comprises a connecting rod 21 connected to the mounting block 11 and an electric rotor 22 mounted on the upper end surface of the connecting rod 21, and the electric rotor 22 is mounted on the upper end surface of the connecting rod 21; the adjustment component 3 comprises a balancing rotor 31 symmetrically arranged on the left and right and electrically connected to the UAV controller 12, and a cross bar 32 mounted on the lower end surface of the body 1, and the balancing rotor 31 is slidably connected to the cross bar 32, It is used to adjust the flight angle of the drone to maintain the balance of the drone by generating reverse wind force when the wind is too strong and causes the drone to shake and cannot maintain a hovering state; a driving component 4, which is arranged on the bottom surface of the body 1 and is transmission-connected to the adjusting component 3 and electrically connected to the drone control, and includes a horizontal adjusting member 41 and an axial adjusting member 42 for driving the balancing rotor 31, so as to adjust the direction of the balancing rotor 31, so that when the drone tilts or shakes violently according to the wind direction, it can be adjusted to a suitable position and angle in time, so that the balancing wind force is generated by the balancing rotor 31 to restore the stability of the drone; a wind resistance cover 5, which is installed on the upper end surface of the wing 2 and surrounds the propeller of the wing 2, and is used to guide the strong wind blowing towards the wing 2 and make it downward along the wing 2, thereby reducing the influence of the strong wind on the electric rotor 22.

[0022] The above design can monitor the wind direction and wind force changes in the flight environment in real time by setting the wind force, wind direction and wind force sensor 13, the adjustment component 3, the drive component 4 and the wind resistance cover 5, and provide accurate data support for the flight control of the UAV. When encountering strong wind or sudden change of wind direction causing the UAV to shake and unable to hover stably, the balance rotor 31 in the adjustment component 3 can respond quickly, adjust its direction and wind force output according to the command of the UAV controller 12, and generate reverse wind force to offset the influence of external wind force, thereby effectively maintaining the balance state of the UAV and improving the flight stability. The flexible adjustment mechanism of the balance rotor 31 enables the UAV to quickly adjust its flight attitude when facing a complex and changeable flight environment, effectively cope with adverse conditions such as strong wind and side wind, and enhance the wind resistance and environmental adaptability of the UAV. The wind resistance cover 5 further reduces the direct impact of strong wind on the electric rotor 22, and effectively reduces the wind resistance by guiding the airflow to flow downward along the wing 2, thereby improving the flight efficiency and heading accuracy of the UAV.

[0023] Furthermore, a through groove 321 is provided on the upper end surface of the cross bar 32, and the front and rear arms of the through groove 321 are symmetrically provided with inwardly recessed grooves 322. A slider 311 is provided on the upper end surface of the balancing rotor 31, and the slider 311 is slidably connected in the through groove 321, and a driving member 33 is provided in the slider 311, and the driving member 33 is used to drive the slider 311 to slide in the through groove 321. When strong wind blows the drone, the driving member 33 is started to drive the slider 311 to move, so that the balancing rotor 31 is adjusted, and the balancing rotor 31 is moved left and right, and the downward pressure generated by the balancing rotors 31 at both ends is matched with the wind force according to the actual wind direction and wind force.

[0024] Furthermore, the upper and lower walls of the groove 322 are provided with staggered racks 323, the driving member 33 includes a dual-axis motor 331 and a first gear 332 meshing with the rack 323, the slider 311 is provided with a mounting chamber 313, the dual-axis motor 331 is installed in the mounting chamber 313, the output end of the dual-axis motor 331 passes through the mounting chamber 313 and extends into the groove 322, the first gear 332 is installed at the output end of the dual-axis motor 331 and meshes with the rack 323, and the upper end surface of the slider 311 is symmetrically provided with an integral The formed L-shaped plate 312, the slider 311 is slidably connected to the outer wall of the cross bar 32 through the L-shaped plate 312, and when in use, the first gear 332 is driven by the motor to rotate the first gear 332 in the rack 323. Since the rack 323 is staggered, when the first gear 332 rotates, it will drive the slider 311 to move, so that the balancing rotor 31 moves forward and backward. When moving, the L-shaped plate 312 is stuck on the outer wall of the cross bar 32, so that when the motor drives the first gear 332 to rotate, the slider 311 can move downward instead of rotating in place following the motor drive shaft.

[0025] Furthermore, the horizontal adjustment member 41 includes a sleeve 411, a connecting plate 412, a mounting column 413, a mounting cylinder 414 and a first motor 415. The first motor 415 is fixedly mounted on the bottom surface of the body 1, and the output shaft of the first motor 415 is arranged downwardly. The sleeve 411 is mounted on the bottom surface of the body 1 and covers the first motor 415. A bearing 418 is installed in the sleeve 411, and the mounting cylinder 414 is installed in the bearing 418. The connecting plate 412 is fixedly mounted on the outer wall of the mounting cylinder 414. The mounting column 413 is symmetrically mounted on the bottom surface of the connecting plate 412. A through hole 416 is provided on the left end surface of the mounting column 413. A rotating shaft 417 is rotatably connected in the through hole 416. The rotating shaft 417 is fixedly connected to the cross bar 32. The other end of the rotating shaft 417 is connected to the axial adjustment member 42, and the axial adjustment member 42 is mounted in the mounting cylinder 414. When in use, the first motor 415 is used to drive the sleeve 411 to rotate, so that the sleeve 411 drives the connecting plate 412 to rotate, the connecting plate 412 drives the mounting column 413 to rotate, and the mounting column 413 drives the cross bar 32 to rotate, so that the balancing rotor 31 can be rotated 360 degrees and adjusted, and can more flexibly generate reverse wind force to offset the influence of external wind force, thereby effectively maintaining the balance state of the drone.

[0026] Furthermore, the axial adjustment member 42 includes a mounting plate 421, a connecting member 422 and a second motor 423. The mounting plate 421 is mounted on the inner wall of the mounting tube 414. The connecting member 422 is arranged on the right end face of the mounting plate 421 and is respectively connected to the symmetrically arranged rotating shafts 417 for transmitting power to simultaneously rotate and adjust the left and right symmetrical cross bars 32. The second motor 423 is connected to the connecting member 422.

[0027] Furthermore, the connecting member 422 includes a mounting seat 424, a second gear 425, a third gear 426 and a connecting shaft 427. The mounting seat 424 is mounted on the right end surface of the mounting plate 421. The second gear 425 is connected to the mounting seat 424 for rotation symmetrically in front and back. The third gear 426 is connected to the mounting seat 424 for rotation symmetrically in left and right. The second gear 425 and the third gear 426 are meshed with each other. The connecting shaft 427 is respectively connected to the outer wall of the second gear 425. The rotating shaft 417 extends into the installation tube 414 and is rotatably connected to the connecting shaft 427. The second motor 423 is fixedly connected to one of the third gears 426. When in use, the third gear 426 is driven by the second motor 423, so that the second gear 425 is driven by the third gear 426. At this time, since the symmetrical second gears 425 are engaged with the third gear 426, when the third gear 426 rotates, the symmetrical second gears 425 rotate in opposite directions, so that the symmetrically arranged cross bars 32 can rotate in opposite directions respectively.

[0028] Furthermore, the wind resistance cover 5 includes a blocking cylinder 51 and a cylindrical fan blade 52, wherein a connecting plate 511 is symmetrically arranged in the blocking cylinder 51, and the connecting plate 511 is fixedly connected to the outer wall of the connecting rod 21, and the outer wall of the blocking cylinder 51 is provided with a plurality of wind guide grooves 512 that penetrate downwardly through the blocking cylinder 51, and the cylindrical fan blade 52 is rotatably connected to the outer wall of the blocking cylinder 51, and the cylindrical fan blade 52 includes a plurality of inclined blades 522 and a mounting ring 521 that is symmetrically arranged up and down, and the mounting ring 521 is rotatably connected to the outer wall of the blocking cylinder 51, and the blade 522 is mounted on the outer wall of the blocking cylinder 51, and the blade 522 is mounted on the outer wall of the blocking cylinder 51. The wind guide grooves 512 are spirally distributed on the outer wall of the blocking cylinder 51. The blocking cylinder 51, as the main windproof structure, can absorb and disperse part of the wind force, and the rotation of the cylindrical fan blades 52 can further guide the airflow, reduce the impact of wind resistance and turbulence on the UAV, thereby significantly improving the flight stability of the UAV. When in use, the wind blows toward the cylindrical fan blades 52, and through the combination of multiple inclined blades 522 and the mounting rings 521 symmetrically arranged up and down, a dynamic structure that can efficiently guide the airflow is formed, thereby effectively reducing wind resistance and enhancing the wind resistance of the UAV.

[0029] It should be noted that the inclination direction of the blade 522 and the spiral setting direction of the guide groove are the same as the rotation direction of the electric rotor 22, so that the derived wind can most effectively reduce wind resistance and enhance the wind resistance of the drone.

[0030] The working principle and use process of the present invention: When the drone takes off and heads, the wind force generated in the air is captured by the wind force, wind direction and wind force sensor 13. When the wind force is strong enough, the wind force, wind direction and wind force sensor 13 transmits a signal to the drone controller 12, so that the drone controller 12 starts the dual-axis motor 331, the first motor 415 and the second motor 423. After the dual-axis motor 331 is started, it drives the first gear 332 to move the slider 311 to adjust the horizontal position of the balancing rotor 31, so that the balancing rotor 31 can generate downward wind force, thereby balancing the body 1 and keeping the body 1 balanced against strong winds. At the same time, the first motor 415 starts to drive the mounting cylinder 414 to rotate, the mounting cylinder 414 drives the connecting disk 412 to rotate, the connecting disk 412 drives the mounting column 413 to rotate, and the mounting column 413 drives the cross bar 32 to rotate, so that the matching rotor rotates with the center point of the connecting disk 412 as the axis. After the second motor 423 is started, it drives the third gear 426 to rotate, and the third gear 426 drives the second gear 425 to rotate, so that the second gear 425 drives The connecting shaft 427 rotates, and the two connecting shafts 427 rotate in opposite directions. The connecting shaft 427 drives the cross bar 32 to rotate, so that the angle and position of the balancing rotor 31 can be flexibly adjusted according to the direction. At the same time, when strong wind contacts the blade 522, it can push the blade 522, so that the blade 522 drives the mounting ring 521 to rotate, forming a dynamic structure that can efficiently guide the airflow, and then enters the blocking cylinder 51, and is guided into the wind guide groove 512 through the blocking cylinder 51, and is spirally transported out of the blocking cylinder 51 through the wind guide groove 512, reducing the impact of wind resistance and turbulence on the drone, thereby significantly improving the flight stability of the drone, so that when encountering strong wind or sudden change in wind direction causing the drone to shake and unable to hover stably, its direction and wind output are adjusted according to the command of the drone controller 12, and reverse wind force is generated to offset the impact of external wind force, thereby effectively maintaining the balance state of the drone, and by guiding the airflow to flow downward along the wing 2, the wind resistance is effectively reduced, and the flight efficiency and heading accuracy of the drone are improved.

Claims

1. A multi-rotor UAV with high-precision heading control, characterized in that: include: A body (1) having wings (2) on its outer wall; An adjustment component (3) comprising a balancing rotor (31) which is symmetrically arranged on both sides and electrically connected to the body (1), and a crossbar (32) mounted on the lower end surface of the body (1), wherein the balancing rotor (31) is slidably connected to the crossbar (32) and is used to adjust the flight angle of the drone to maintain the balance of the drone by generating reverse wind force when the drone vibrates and cannot maintain a hovering state due to excessive wind force; A driving assembly (4) is arranged on the bottom surface of the body (1) and is transmission-connected to the adjustment assembly (3) and electrically connected to the body (1), and comprises a horizontal adjustment member (41) and an axial adjustment member (42) for driving the balancing rotor (31), thereby adjusting the orientation of the balancing rotor (31) so that when the UAV tilts or shakes violently according to the wind direction, the UAV is promptly adjusted to a suitable position and angle, thereby generating a balancing wind force through the balancing rotor (31) to restore stability of the UAV; A wind resistance cover (5) is installed on the upper end surface of the wing (2) and surrounds the propeller of the wing (2), and is used to guide the strong wind blowing towards the wing (2) and make it go downward along the wing (2), thereby reducing the impact of the strong wind on the wing (2).

2. A multi-rotor UAV with high-precision heading control according to claim 1, characterized in that: The upper end surface of the cross bar (32) is provided with a through groove (321), and the front and rear arms of the through groove (321) are symmetrically provided with inwardly recessed grooves (322). The upper end surface of the balancing rotor (31) is provided with a slider (311), and the slider (311) is slidably connected in the through groove (321), and a driving member (33) is provided in the slider (311), and the driving member (33) is used to drive the slider (311) to slide in the through groove (321).

3. A multi-rotor UAV with high-precision heading control according to claim 2, characterized in that: The upper and lower walls of the groove (322) are provided with staggered racks (323); the driving member (33) comprises a dual-axis motor (331) and a first gear (332) meshing with the rack (323); a mounting chamber (313) is provided in the slider (311); the dual-axis motor (331) is mounted in the mounting chamber (313); the output end of the dual-axis motor (331) passes through the mounting chamber (313) and extends into the groove (322); the first gear (332) is mounted on the output end of the dual-axis motor (331) and meshes with the rack (323); an upper end surface of the slider (311) is symmetrically provided with an integrally formed L-shaped plate (312); the slider (311) is slidably connected to the outer wall of the crossbar (32) via the L-shaped plate (312).

4. A multi-rotor UAV with high-precision heading control according to claim 3, characterized in that: The horizontal adjustment member (41) comprises a sleeve (411), a connecting plate (412), a mounting column (413), a mounting cylinder (414), and a first motor (415); the first motor (415) is fixedly mounted on the bottom surface of the machine body (1), and the output shaft of the first motor (415) is arranged downward; the sleeve (411) is mounted on the bottom surface of the machine body (1) and covers the first motor (415); a bearing (418) is installed in the sleeve (411); and the mounting cylinder (414) is mounted on the bearing (418). ), the connecting disk (412) is fixedly mounted on the outer wall of the mounting tube (414), the mounting column (413) is symmetrically mounted on the bottom surface of the connecting disk (412), the left end surface of the mounting column (413) is provided with a through hole (416), a rotating shaft (417) is rotatably connected in the through hole (416), the rotating shaft (417) is fixedly connected to the cross bar (32), the other end of the rotating shaft (417) is connected to the axial adjustment member (42), and the axial adjustment member (42) is mounted in the mounting tube (414).

5. A multi-rotor UAV with high-precision heading control according to claim 4, characterized in that: The axial adjustment member (42) comprises a mounting plate (421), a connecting member (422) and a second motor (423); the mounting plate (421) is mounted on the inner wall of the mounting tube (414); the connecting member (422) is arranged on the right end surface of the mounting plate (421) and is respectively connected to symmetrically arranged rotating shafts (417) for transmitting power to simultaneously rotate and adjust the left and right symmetrical cross bars (32); and the second motor (423) is connected to the connecting member (422).

6. A multi-rotor UAV with high-precision heading control according to claim 5, characterized in that: The connecting member (422) comprises a mounting seat (424), a second gear (425), a third gear (426) and a connecting shaft (427); the mounting seat (424) is mounted on the right end surface of the mounting plate (421); the second gear (425) is connected to the mounting seat (424) in a manner of symmetrically rotating frontward and rearward; the third gear (426) is connected to the mounting seat (424) in a manner of symmetrically rotating leftward and rightward; the second gear (425) and the third gear (426) are meshed with each other; the connecting shaft (427) is respectively connected to the outer walls of the symmetrical second gears (425); the rotating shaft (417) extends into the mounting tube (414) and is rotatably connected to the connecting shaft (427); and the second motor (423) is fixedly connected to one of the third gears (426).

7. The multi-rotor UAV with high-precision heading control according to claim 1, characterized in that: A plurality of mounting blocks (11) for mounting the wing (2) are symmetrically arranged on the outer wall of the body (1), and the upper end surfaces of the mounting blocks are respectively provided with a drone controller (12) and a wind direction and wind force sensor (13), the wind direction and wind force sensor (13) being electrically connected to the drone controller (12), and the wing (2) comprises a connecting rod (21) connected to the mounting block (11) and an electric rotor (22) mounted on the upper end surface of the connecting rod (21), and the electric rotor (22) is mounted on the upper end surface of the connecting rod (21).

8. The multi-rotor UAV with high-precision heading control according to claim 7, characterized in that: The outer wall of the electric rotor (22) is provided with a wind resistance cover (5), which is mounted on the upper end surface of the wing (2) and surrounds the propeller of the wing (2) and is used to guide strong wind blowing toward the wing (2) and make it flow downward along the wing (2), thereby alleviating the influence of the strong wind on the electric rotor (22). The wind resistance cover (5) comprises a blocking cylinder (51) and cylindrical blades (52), and the blocking cylinder (51) is symmetrically provided with connecting plates (511), and the connecting plates (511) are fixedly connected to the outer wall of the connecting rod (21). The outer wall of the blocking cylinder (51) is provided with a plurality of wind guide grooves (512) penetrating downwardly through the blocking cylinder (51), and the cylindrical blades (52) are rotatably connected to the outer wall of the blocking cylinder (51).

9. A multi-rotor UAV with high-precision heading control according to claim 8, characterized in that: The cylindrical fan blade (52) comprises a plurality of blades (522) arranged obliquely and mounting rings (521) arranged symmetrically up and down, the mounting rings (521) being rotatably connected to the outer wall of the blocking cylinder (51), and the blades (522) being mounted between the mounting rings (521) arranged symmetrically up and down.

10. A multi-rotor UAV with high-precision heading control according to claim 9, characterized in that: The air guide grooves (512) are spirally distributed on the outer wall of the blocking cylinder (51).

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